Improved test method and analytical modelling for fatigue crack growth in coarse-grain titanium alloy with rough fatigue surfaces-Reference-Cited by-同舟云学术

Improved test method and analytical modelling for fatigue crack growth in coarse-grain titanium alloy with rough fatigue surfaces

Published:2014-02-19 Issue:6 Volume:37 Page:659-670
ISSN:8756-758X
Container-title:Fatigue & Fracture of Engineering Materials & Structures
language:en
Short-container-title:Fatigue Fract Engng Mater Struct

Author:

Walker K. F.¹²,Newman J. C.³

Affiliation:

1. Defence Science Technology Organisation; Fishermans Bend Vic. Australia

2. RMIT University; Bundoora Vic. Australia

3. Aerospace Engineering; Mississippi State University; Mississippi State MS USA

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Link

http://onlinelibrary.wiley.com/wol1/doi/10.1111/ffe.12148/fullpdf

Reference23 articles.

1. Walker , K. Walliker , A. Meadows , L. Matricciani , E. 2012 A comprehensive testing and analytical model development program to assure ongoing structural integrity of the aging Australian P-3C fleet Aircraft Airworthiness and Sustainment Conference

2. Wallbrink , C. Jackson , P. Hu , W. 2011 Crack grwoth rate curves: which part dominates life prediction and when? International Committee on Aeronautical Fatigue

3. A method for determining the stress intensity threshold level for fatigue crack propagation;Ohta;Eng. Fract. Mech.,1977

4. Minakawa , K. McEvily , A. J. 1981 On near-threshold fatigue crack growth in steels and aluminum alloys International Conference on Fatigue Thresholds

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